Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams December 2013 – 04-BS-6: Mechanics of Materials
3 hours duration, closed book (one hand-written aid sheet permitted). Any five of the eight
questions constitute a complete paper; all eight are solved below as a complete study resource.
Reference texts: R.C. Hibbeler, Mechanics of Materials, 10th ed.
(Ch. 5 torsion, Ch. 6 shear/moment diagrams & composite beams, Ch. 7 transverse shear,
Ch. 8 combined loadings, Ch. 9 stress transformation, Ch. 12 deflection by integration,
Ch. 13 buckling); F. Beer & E.R. Johnston, Mechanics of Materials; W. Gere &
B. Goodno, Mechanics of Materials (alternates). A W-shape properties table printed on
the exam's last page is not needed — every question supplies its own section dimensions.
Stepped aluminum shaft, fixed at E; torques at A (25 CW), B (30 CCW), C (35 CW) kN·m.
Given.
Segment
Length (mm)
Diameter (mm)
AB
500
100 (solid)
BC
300
60 (solid)
CD
400
120 (solid)
DE
800
120 OD / 60 ID (hollow)
G = 25 GPa; TA=25 kN·m (CW), TB=30 kN·m (CCW),
TC=35 kN·m (CW); shaft fixed at E.
Find. (a) Maximum shear stress and its radial variation. (b) Angle of twist
of A relative to the fixed end E. (c) The effect of doubling all three torques.
Approach. Take clockwise as positive; find the internal torque in each of the
four segments by summing the applied torques to the free (A) side of each cut, then apply
$\tau=Tr/J$ and $\phi=TL/(GJ)$ segment by segment, summing the angles algebraically.
Internal torque in each segment (CW+).
$$T_{AB}=T_A=+25, \quad T_{BC}=T_A+T_B=25-30=-5, \quad T_{CD}=T_{DE}=T_A+T_B+T_C
=25-30+35=+30\ [\text{kN}\cdot\text{m}]$$
Part (a): shear stress in each segment, at its outer radius.
$$\tau_{AB}=\frac{T_{AB}r_{AB}}{J_{AB}}=\frac{25\times10^6(50)}{9.817\times10^6}
=\boxed{127.3\ \text{MPa}}\ \text{(governs)}$$
$$\tau_{BC}=117.9\ \text{MPa}, \qquad \tau_{CD}=88.4\ \text{MPa}, \qquad
\tau_{DE}=94.3\ \text{MPa}$$
Segment AB governs at $\tau_{max}=127.3$ MPa ($<200$ MPa yield, OK). In every segment τ
varies LINEARLY from zero at the shaft's centre to this maximum at the outer radius (for the
hollow segment DE, from a non-zero value at the 30 mm inner radius up to the maximum at the
60 mm outer radius).
Part (b): angle of twist, A relative to E. Sum $\phi_i=T_iL_i/(GJ_i)$
(signed, CW+) over all four segments (G = 25{,}000 MPa):
$$\phi_{AB}=+2.918^\circ, \ \phi_{BC}=-2.702^\circ, \ \phi_{CD}=+1.351^\circ,
\ \phi_{DE}=+2.882^\circ$$
$$\boxed{\phi_{A/E}=\Sigma\phi_i = +4.45^\circ}\ \text{(net clockwise, viewed from A)}$$
Part (c): doubling all three torques. The shaft remains linear-elastic as
long as no segment yields, so both τ and φ scale directly with T: every stress and the
total twist would exactly DOUBLE (new $\tau_{max}=254.6$ MPa, new $\phi=8.90^\circ$).
However $254.6\ \text{MPa} > 200\ \text{MPa}$ (yield), so segment AB (and possibly BC) would
actually begin to YIELD; the true response would become elastic-plastic and the simple
doubling relationship would no longer hold once yielding starts.
Final Results.
Quantity
Value
TAB, TBC, TCD=TDE
+25, −5, +30 kN·m
(a) τmax
127.3 MPa, in segment AB
(b) φA/E
4.45°, clockwise
(c) Loads doubled
τ, φ would double if still elastic, but 254.6 MPa > 200 MPa yield → AB yields, no longer proportional